Fuselage rear end of an aircraft
Fuselage rear end of an aircraft, comprising: - a structural part (1) comprising a skin and longitudinal (30) and transversal reinforcing members (31, 32), and - a fairing (5). The structural part (1) longitudinally spans over the whole rear end and comprises a first portion (2) in which the transve...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | Fuselage rear end of an aircraft, comprising:
- a structural part (1) comprising a skin and longitudinal (30) and transversal reinforcing members (31, 32), and
- a fairing (5). The structural part (1) longitudinally spans over the whole rear end and comprises a first portion (2) in which the transversal reinforcing members (32) occupy the whole perimeter of the corresponding fuselage section and at least a second portion (3) in which the transversal reinforcing members (31) occupy only a portion of the perimeter of the corresponding fuselage section, the fairing (5) being located below the second portion (3) of the structural part (1). |
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